# Service difficulty reports: N604CZ

A list on [N604CZ](https://openairdocs.org/aircraft/N604CZ.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 3 · 129 reports

- [SDR SWIA2026070976749](https://openairdocs.org/sdr/SWIA2026070976749.md): Shear Tie · corroded · Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED IN AFT CARGO BAY, FR 76 BTWN S28R-29R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08.
- [SDR SWIA2026070976748](https://openairdocs.org/sdr/SWIA2026070976748.md): Shear Tie · corroded · Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED IN AFT CARGO BAY, FR 75, BTWN S28L-29L. REMOVED & REPLACED THE SHEAR TIE IAW SRM 51-40-08.
- [SDR SWIA2026070976745](https://openairdocs.org/sdr/SWIA2026070976745.md): Shear Tie · corroded · Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT AFT CARGO FR 74, STR 29L-29R. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-40-08.
- [SDR SWIA2026070976744](https://openairdocs.org/sdr/SWIA2026070976744.md): Shear Tie · corroded · Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT AFT CARGO FR 75, STR 29R-28R. REMOVED AND REPLACED THE SHEAR TIE IAW SRM 51-40-08.
- [SDR SWIA2026070976743](https://openairdocs.org/sdr/SWIA2026070976743.md): Shear Tie · corroded · Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT AFT CARGO FR 75, STR 29L-29R. REMOVED AND REPLACED THE SHEAR TIE, FR 75, STR 29L-29R IAW SRM 51-40-08.
- [SDR SWIA2026070976741](https://openairdocs.org/sdr/SWIA2026070976741.md): Shear Tie · corroded · Jul 9, 2026 · N604CZ · Emb ERJ170200LR · Fuselage Internal Mounting Structure
  > SHEAR TIE CORRODED AT AFT CARGO FR 74, STR 28R-29R. REMOVED AND REPLACED SHEAR TIE IN AFT CARGO FR 74 STR 28R-29R. IAW SRM 51-40-08. SEE CONTINUE CARD FOR WORK PERFORMED.
- [SDR SWIA2026070876751](https://openairdocs.org/sdr/SWIA2026070876751.md): Seat Track · nicked · Jul 8, 2026 · N604CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT LATERAL SEAT TRACK HAS MULTIPLE NICKS AND SCRATCHES, FR 23-34. REMOVED AND REPLACED THE LT LATERAL SEAT TRACK IAW SRM 51-40-08.
- [SDR SWIA2026070876747](https://openairdocs.org/sdr/SWIA2026070876747.md): Seat Track · nicked · Jul 8, 2026 · N604CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT INBD SEAT TRACK HAS NICKS AND SCRATCHES AT MULTIPLE LOCATIONS, FR 23-32. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-08.
- [SDR SWIA2026070876746](https://openairdocs.org/sdr/SWIA2026070876746.md): Seat Track · damaged · Jul 8, 2026 · N604CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > LEFT INBD SEAT TRACK HAD MULTIPLE LOCATIONS OF BARE METAL, BETWEEN FRAMES 43 & 59. R & R LT INBD SEAT TRACK IAW SRM 51-40-08.
- [SDR SWIA2026070876742](https://openairdocs.org/sdr/SWIA2026070876742.md): Seat Track · damaged · Jul 8, 2026 · N604CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT, INBD SEAT TRACK HAD MULTIPLE LOCATIONS OF BARE METAL BETWEEN FRAME 43 AND FRAME 59. REMOVED AND REPLACED THE RT INBD SEAT TRACK IAW SRM 51-40-08. REPLACED WITH OEM PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARDS AND TASK CARDS FOR FURTHER
- [SDR SWIA2026070776753](https://openairdocs.org/sdr/SWIA2026070776753.md): Flap Track · out of limits · Jul 7, 2026 · N604CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > LEFT NR 1A FLAP TRACK HAS DEPTH REDUCTION OF.50 MM AT DEEPEST MEASUREMENT. REMOVED AND REPLACED LT, #1A FLAP TRACK IAW AMM 57-54-25 OPS CHECK GOOD IAW AMM 27-50-00.
- [SDR SWIA2026070776752](https://openairdocs.org/sdr/SWIA2026070776752.md): Flap Track · out of limits · Jul 7, 2026 · N604CZ · Emb ERJ170200LR · Trailing Edge Flaps
  > RIGHT NR 5 FLAP TRACK HAS DEPTH REDUCTION OF.80 MM AT DEEPEST MEASUREMENT. REMOVED AND REPLACED THE RT NR 5 FLAP TRACK IAW AMM 27-51-08.
- [SDR SWIA2026070676750](https://openairdocs.org/sdr/SWIA2026070676750.md): Skin · cracked · Jul 6, 2026 · N604CZ · Emb ERJ170200LR · Wing, Plate/Skin
  > RIGHT WING FIXED LEADING EDGE IS CRACKED AT SLAT 2 INBD TRACK UPPER CUTOUT. PERFORMED DOUBLER REPAIR ON RT WING FIXED LEADING EDGE AT SLAT 2 INBD TRACK UPPER CUTOUT. IAW ETD2026-170-012023-B.
- [SDR REXA2024100100765](https://openairdocs.org/sdr/REXA2024100100765.md): Power Unit · inoperative · Sep 24, 2024 · N604CZ · Emb ERJ170200LR · Emergency Lighting
  > EMERGENCY LIGHT BATT FAULT FAULT CODE: 33500003UT1 R&R POWER UNIT IAW AMM 33-50-01 OPS TEST GOOD AT THIS TIME PN OFF/ON 3400-22-10 SN OFF - 003342 SN ON - 002392
- [SDR SWIA202266380](https://openairdocs.org/sdr/SWIA202266380.md): None · damaged · Jun 29, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Frame
  > TOOLING MARK IN FRAME 89 BELOW SHEAR CLIP BETWEEN STRINGERS 28R - 27R. (C-CHECK RO 8/29/2022) REPAIRED FR89 BETWEEN STGRS 27R-28R. REF ETD 2022-170-022186. SEE CONTINUATION FOR WORK PERFORMED. SEE CAMP # 25042797 FOR PRESSURIZATION CHECK. REPAIR PARTS W
- [SDR SWIA202266379](https://openairdocs.org/sdr/SWIA202266379.md): None · worn · Jun 27, 2022 · N604CZ · Emb EMB110* · Stabilizer Position Indicating
  > HORIZONTAL STABILIZER, LH FRAME 100 HINGE POINT, BUSHING BORE HAS WEAR/SCORING AND CORROSION (C-CHECK RO 8/29/2022) TEMPORARY REPAIR OF LH FRAME 100 HINGE POINT, BUSHING BORE BY REAMING, BUSHING FABRICATION AND INSTALLATION REF ETD 2022-170-021921 REV
- [SDR SWIA202266378](https://openairdocs.org/sdr/SWIA202266378.md): None · corroded · Jun 23, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > SHEAR CLIP HAS CORROSION AT FR 89 STR 28R-27R. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED SHEAR CLIP AT FR 89 STR 28R-27R REF SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202266377](https://openairdocs.org/sdr/SWIA202266377.md): None · corroded · Jun 22, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > CENTER FUSELAGE III FRAME 83 CORRODED SHEAR CLIP STRINGERS 28R/29R. (C-CHECK RO 8/29/2022) / REMOVED AND REPLACED CENTER FUSELAGE III FRAME 83 SHEAR CLIP AT STRINGERS 28R/29R REF SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE
- [SDR SWIA202266376](https://openairdocs.org/sdr/SWIA202266376.md): None · corroded · Jun 22, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > CENTER FUSELAGE III FRAME 82 CORRODED UNDER SHEAR CLIP STRINGER 27R/28R. (C-CHECK RO 8/29/2022) / REMOVED AND REPLACED CENTER FUSELAGE III FRAME 82 REF: SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD F
- [SDR SWIA202266375](https://openairdocs.org/sdr/SWIA202266375.md): None · corroded · Jun 22, 2022 · N604CZ · Emb EMB110* · Fuselage Structure (General)
  > CENTER FUSELAGE III SKIN CORRODED UNDER FRAME 82 SHEAR CLIP STRINGER 27R/28R. (C-CHECK RO 8/29/2022) / CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED CUTOUT, FILLER, INNER AND OUTER DOUBLER REPAIR REF SRM 53-23-01/REPAIR13P. SEE CONTINUATION CARD FOR W
- [SDR SWIA202266374](https://openairdocs.org/sdr/SWIA202266374.md): None · corroded · Jun 22, 2022 · N604CZ · Emb EMB110* · Fuselage Structure (General)
  > COCKPIT RH FLOOR STRUCTURE DOUBLER CORRODED AT SEVERAL AREAS AS MARKED (C-CHECK RO 8/29/2022) / PERFORMED REPAIR OF COCKPIT RH FLOOR STRUCTURE DOUBLER REF ETD2022-170-021607. 102.4 GRAMS ADDED FROM REPAIR, NO CHANGE TO WEIGHT AND BLANCE REQUIRED
- [SDR SWIA202266373](https://openairdocs.org/sdr/SWIA202266373.md): None · corroded · Jun 22, 2022 · N604CZ · Emb EMB110* · Fuselage Structure (General)
  > COCKPIT LH FLOOR STRUCTURE DOUBLER CORRODED AT SEVERAL FASTENERS AS MARKED (C-CHECK RO 8/29/2022) / REPAIRED COCKPIT LH FLOOR STRUCTURE DOUBLER BY SPLICING A NEW SECTION IN FROM FR 7 TO FR 12 AND RESTORED SURFACE PROTECTION REF ETD 2022-170-021533
- [SDR SWIA202266372](https://openairdocs.org/sdr/SWIA202266372.md): None · corroded · Jun 22, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Frame
  > COCKPIT FLOOR STRUCTURE CENTER CROSS BEAM AT FRAME 11 CORRODED AS MARKED / (C-CHECK RO 8/29/2022) BLENDED COCKPIT FLOOR STRUCTURE CROSS BEAM AT FR 11 2EA LOCATIONS. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-10-10/AD02. ASSET#:TC2-8911 CAL DUE:11-9-22
- [SDR SWIA202266371](https://openairdocs.org/sdr/SWIA202266371.md): None · corroded · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Frame
  > CORROSION CENTER FUSELAGE III FRAME 80 JUST OUTBOARD OF STRINGER 28R CORRODED. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED CENTER FUSELAGE III FRAME 80 R/H LOWER SECTION REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. FRAME 80 REPLACED WITH
- [SDR SWIA202266370](https://openairdocs.org/sdr/SWIA202266370.md): None · corroded · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO R/H FR 83 BETWEEN STGR 27R / 28R SHEAR CLIP CORRODED. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED AFT CARGO R/H FR 83 BETWEEN STGR 27R / 28R SHEAR CLIP REF SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUA
- [SDR SWIA202266369](https://openairdocs.org/sdr/SWIA202266369.md): None · corroded · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO R/H SHEAR CLIP AT FR 85 STGR 27R TO 28R CORRODED AS MARKED. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED AFT CARGO R/H SHEAR CLIP AT FR 85 STGR 27R TO 28R. REF ERJ175 SRM 51-4-08. RESTORED SURFACE PROTECTION. REPLACED WITH FACTORY PART, NO CHAN
- [SDR SWIA202266368](https://openairdocs.org/sdr/SWIA202266368.md): None · corroded · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO R/H SHEAR CLIP AT FR 84 STGR 27R TO 28R CORRODED AS MARKED. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED AFT CARGO R/H SHEAR CLIP AT FR 84 STGR 27R TO 28R REF SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTIN
- [SDR SWIA202266367](https://openairdocs.org/sdr/SWIA202266367.md): None · corroded · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO R/H SHEAR CLIP AT FR 82 STGR 28R TO 29R CORRODED AS MARKED (C-CHECK RO 8/29/2022) REMOVED AND REPLACED AFT CARGO R/H SHEAR CLIP AT FR 82 STGR 28R TO 29R REF:SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINU
- [SDR SWIA202266366](https://openairdocs.org/sdr/SWIA202266366.md): None · corroded · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > SHEAR CLIP AT FR.84 BETWEEN STR. 28R-29R HAS CORROSION. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED SHEAR CLIP AT FR.84 BETWEEN STR. 28R-29R REF SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PE
- [SDR SWIA202266365](https://openairdocs.org/sdr/SWIA202266365.md): None · scratched · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > R/H INBD SEAT TRACK HAS NUMEROUS SCRATCHES,CHAFE MARKS AND AREAS OF BARE METAL FRAMES 74 THROUGH 80. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED R/H INBD SEAT TRACK FR74-84 REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. SEAT TRACK REPLACED
- [SDR SWIA202266364](https://openairdocs.org/sdr/SWIA202266364.md): None · scratched · Jun 21, 2022 · N604CZ · Emb EMB110* · Fuselage, Powerplant Attach Fittings
  > L/H INBD SEAT TRACK HAS NUMEROUS SCRATCHES,CHAFE MARKS AND AREAS OF BARE METAL FRAMES 74 THROUGH 80. (C-CHECK RO 8/29/2022) BLENDED SEVERAL SPOTS ON L/H IB SEAT TRACK FR 74-80, FOUND WITHIN LIMITS REF EMB SRM 53-23-10/AD01. / AT FR 78-79, AND FR 82-83
- [SDR SWIA202266363](https://openairdocs.org/sdr/SWIA202266363.md): None · cracked · Jun 20, 2022 · N604CZ · Emb EMB110* · Doors
  > FORWARD PAX DOOR FORWARD UPPER SEAL DEPRESSOR ON THE FUSELAGE CRACKED. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED FORWARD PAX DOOR FORWARD UPPER SEAL DEPRESSOR REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA202266362](https://openairdocs.org/sdr/SWIA202266362.md): None · corroded · Jun 19, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > CORROSION- SHEARCLIP FRAME 86 STRINGERS 27R/28R. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP ON FR 86 STGR 27-28R. RESTORED SURFACE PROTECTION IAW SRM 51-23-06. RESTORED CIC IAW CPM 51-25-00-910-001-A. REPLACED WITH FACTORY PART, NO
- [SDR SWIA202266361](https://openairdocs.org/sdr/SWIA202266361.md): None · corroded · Jun 19, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > CORROSION- FRAME 87 STRINGERS 27R/28R SHEARCLIP. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP ON FRAME 87 STGR 27-28R IAW SRM 51-40-08. RESTORED SURFACE PROTECTION AND CIC IAW SRM 51-23-06 AND CPM 51-25-00-910-001-A. REPLACED WITH FAC
- [SDR SWIA202266360](https://openairdocs.org/sdr/SWIA202266360.md): None · corroded · Jun 19, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > CORROSION- FRAME 88 STRINGERS 27R/28R SHEARCLIP. (C-CHECK RO 8/29/2022) REMOVED AND REPLACED CORRODED SHEAR CLIP ON FR 88 STGR 27-28R IAW SRM 51-40-08. RESTORED SURFACE PROTECTION AND CIC IAW SRM 51-23-06 AND CPM 51-25-00-910-001-A. REPLACED WITH FACTOR
- [SDR SWIA202266359](https://openairdocs.org/sdr/SWIA202266359.md): None · corroded · Jun 18, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO R/H FR 82 BETWEEN STGR 28R / 27R SHEAR CLIP CORRODED. (C-CHECK RO 8/29/2022) / REMOVED AND REPLACED AFT CARGO R/H FR 82 BETWEEN STGR 28R / 27R SHEAR CLIP REF: SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE.
- [SDR SWIA202266358](https://openairdocs.org/sdr/SWIA202266358.md): None · corroded · Jun 18, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > AFT CARGO R/H FR 81 STGR 27R SHEAR CLIP CORRODED. (C-CHECK RO 8/29/2022) / REMOVED AND REPLACED AFT CARGO R/H FR 81 STGR 27R SHEAR CLIP REF SRM 51-40-08. REPLACED WITH FACTORY PART, NO CHANGE TO WEIGHT AND BALANCE. SEE CONTINUATION CARD FOR WORK PERFOR
- [SDR SWIA202266357](https://openairdocs.org/sdr/SWIA202266357.md): None · corroded · Jun 18, 2022 · N604CZ · Emb EMB110* · Fuselage Main, Longeron/Stringer
  > SHEAR CLIP IN FWD CARGO CORRODED AT FRAME 22 BETWEEN STRINGERS 28L-28R (C-CHECK RO 8/29/2022) / REMOVED AND REPLACED SHEAR CLIP IN FWD CARGO AT FRAME 22 BETWEEN STRINGERS 28L-28R REF SRM 51-40-08. SEE CONTINUATION CARD FOR WORK PERFORMED. REPLACED WITH
- [SDR SWIA202266356](https://openairdocs.org/sdr/SWIA202266356.md): None · cracked · Jun 16, 2022 · N604CZ · Emb EMB110* · Wing Structure
  > RH WING LOWER SKIN PANEL HAS SUSPECTED CRACK AT FASTENER HOLE OF DOUBLER OTBD OF RIB 5; ADJACENT FWD GEAR TRUNNION FITTING; MARKED. (C-CHECK RO 8/29/2022) REPAIRED RH WING LOWER SKIN PANEL CRACK AT FASTENER HOLE OF DOUBLER OTBD OF RIB 5; ADJACENT FWD GE
- [SDR SWIA202265570](https://openairdocs.org/sdr/SWIA202265570.md): None · failed · May 7, 2022 · N604CZ · Emb EMB110* · Landing Gear Door Actuator
  > LG LEVER DISAG WARNING MESSAGE WITH RED INDICATIONS ON THE GEAR ON DEPARTURE. COMPLIED WITH QRH AND CYCLED THE HANDLE. GEAR CYCLED NORMALLY AND RETURNED TO FIELD WITH NO FURTHER ISSUES. (FLIGHT 4114 - FILED CLOSED)REMOVED AND REPLACED LANDING-GEAR CONTROL LE
- [SDR C77A2019070800001](https://openairdocs.org/sdr/C77A2019070800001.md): Battery · discharged · Jul 2, 2019 · N604CZ · Emb ERJ170200LR · Emergency Equipment
  > R2 DOOR FA FLASHLIGHT NOT CHARGING AND SEAL BROKEN. R+R FLASHLIGHT BATTERY IAW AMM 35-51-01 REPLACED SECURITY STRAP IAW AMM 35-31-01 OPS CHECK GOOD THIS CLOSES DM2681681 PLACARD REMOVED SDI UPDATED MXC NOTIFIED AC OK FOR SERIVCE.
- [SDR C77A2019042900002](https://openairdocs.org/sdr/C77A2019042900002.md): Battery · defective · Apr 26, 2019 · N604CZ · Emb ERJ170200LR · Emergency Equipment
  > AFT FA FLASHLIGHT INDICATOR IS NOT FLASHING. DEFFERED AFT FA FLASHLIGHT IAW MEL 25-62-02 PER MXC E WELLS #F66158 TRANSFERED TO SDI PLACARD. MEL 25-62-07-1 CAT C: AFT FA FLASHLIGHT INDICATOR IS NOT FLASHING. TROUBLESHOOT FLASHLIGHT AND REMOVED AND REPLACED
- [SDR C77A2019032000001](https://openairdocs.org/sdr/C77A2019032000001.md): Threshold · corroded · Mar 20, 2019 · N604CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > DURING THE CURRENT B6 BASIC CHECK AT EAMS, CORROSION DAMAGE WAS DISCOVERED ON THE AFT PASSENGER (L2) DOOR LOWER THRESHOLD BEAM (P/N 170-65703-005) AT FASTENER HOLES AROUND THE FORWARD AND AFT GIRT BAR FITTINGS DURING ACCOMPLISHMENT OF EO E175-5300-221.2 FOR A
- [SDR C77A2019031400003](https://openairdocs.org/sdr/C77A2019031400003.md): Seat Track · corroded · Mar 14, 2019 · N604CZ · Emb ERJ170200LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH A PERMANENT REPAIR OF CORROSION DAMAGE TO THE CENTER FUSELAGE II FLOOR STRUCTURE RT INBOARD SEAT TRACK P/N 170-86082-003 BY SPLICE REPAIR PER ETD2019-170-032004 AND SRM PART II 53-00-10/REPAIR 01P.
- [SDR C77A2019031100001](https://openairdocs.org/sdr/C77A2019031100001.md): Seat Track · corroded · Mar 12, 2019 · N604CZ · Emb ERJ170100LR · Fuselage, Seat/Cargo Attach Fittings
  > THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE ON CONDITION REPLACEMENT OF A DAMAGED OR PREVIOUSLY REPAIRED RT FLOOR TRACK P/N 170-03263-001 BETWEEN FRAMES 12 AND 20 WITH A NEW P/N 170-03263-001 FLOOR TRACK. THE FLOOR TRACK WILL BE REPLACED
- [SDR C77A2020032670001](https://openairdocs.org/sdr/C77A2020032670001.md): Gusset · corroded · Mar 11, 2019 · N604CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EOE175-5300-231-THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: LH UPPER SHEET P/N 170-86101-001, LH PANEL SUPPORT P/N 170-86139-005, CENTER SHEA
- [SDR C77A2020032600039](https://openairdocs.org/sdr/C77A2020032600039.md): Gusset · corroded · Mar 11, 2019 · N604CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EOE175-5300-231-THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: LH UPPER SHEET P/N 170-86101-001, LH PANEL SUPPORT P/N 170-86139-005, CENTER SHEA
- [SDR C77A2020032600040](https://openairdocs.org/sdr/C77A2020032600040.md): Panel Support · corroded · Mar 11, 2019 · N604CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EOE175-5300-231-THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: LH UPPER SHEET P/N 170-86101-001, LH PANEL SUPPORT P/N 170-86139-005, CENTER SHEA
- [SDR C77A2020032600038](https://openairdocs.org/sdr/C77A2020032600038.md): Shear Panel · corroded · Mar 11, 2019 · N604CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EO E175-5300-231-THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: LH UPPER SHEET P/N 170-86101-001, LH PANEL SUPPORT P/N 170-86139-005, CENTER SHE
- [SDR C77A2020032600037](https://openairdocs.org/sdr/C77A2020032600037.md): Shear Panel · corroded · Mar 11, 2019 · N604CZ · Emb ERJ170200LR · Fuselage Miscellaneous Structure
  > EOE175-5300-231-THIS EO IS BEING ISSUED TO PROVIDE INSTRUCTIONS TO ACCOMPLISH THE PERMANENT REPAIRS OF CORROSION DAMAGE BY REPLACEMENT OF THE FOLLOWING AFT CABIN FLOOR STRUCTURE: LH UPPER SHEET P/N 170-86101-001, LH PANEL SUPPORT P/N 170-86139-005, CENTER SHEA

Next page: https://openairdocs.org/aircraft/N604CZ/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N604CZ' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N604CZ/reports

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